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WO/2011/117521 |
The invention relates to a turboshaft engine supporting pylon covered with a porous material and to a turboshaft engine/pylon assembly. More specifically, the invention relates to a pylon (2) supporting a turboshaft engine (1) on an airc...
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WO/2011/117434 |
The invention relates to a joint system of rescue and provision supply capsules (2, 2') for aircraft in general. The present invention relates to the field of the art aimed at substantially reducing the consequences of an aviation disast...
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WO/2011/116982 |
A sanitary module arrangement (100) suitable for installation in an aircraft cabin comprises a sanitary module (10), the interior (14) of which is separated by a partition wall (12) from an area (16) of the aircraft cabin adjacent to the...
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WO/2011/119720 |
A system is provided, including at least one floor panel adapted to matingly engage and be supported by a support structure; and securing means for securing at least one seat support to the floor panel; wherein the seat support correspon...
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WO/2011/117142 |
The invention relates to an aircraft having at least one air supply channel (14) and at least one exhaust air channel (15) and at least one seat (2) comprising at least one seat frame (25) by means of which the seat is fastened to a part...
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WO/2011/119283 |
A semi -levered landing gear (10) is provided that includes a shock strut (12), a truck beam (18) pivotally connected to the shock strut and a semi -levered landing gear mechanism including at least three links (24, 30a, 30b) configured ...
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WO/2011/118558 |
Provided are a cap which prevents situations where sparks are generated internally even if lightning current flows through a fastener, thereby improving safety; a fastened structure using this cap; and an aircraft having this fastened st...
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WO/2011/116888 |
The invention relates to a seat attachment device, in particular an airline passenger seat attachment device, for the movable fastening of an object (12) to a seat (14), comprising a supporting arm part (16), a device receiving part (18)...
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WO/2011/116888 |
The invention relates to a seat attachment device, in particular an airline passenger seat attachment device, for the movable fastening of an object (12) to a seat (14), comprising a supporting arm part (16), a device receiving part (18)...
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WO/2011/117619 |
An aerial vehicle is described which comprises: a first compartment (13) for holding a lighter than air gas; a second compartment (6, 4) for holding atmospheric air and having an inlet and an outlet; a solar panel (41) for converting sun...
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WO/2011/117610 |
A fuel system comprising a fuel tank (1), a vent tank (3) having a duct open to the ambient atmosphere, a first vent line (4, 5) fluidically connecting the fuel tank ullage to the vent tank (3), a gas drying system (8) including a pump (...
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WO/2011/117863 |
A portable aircraft landing system, comprises an inflatable mat provided with gas outlets, in cooperation with inflation apparatus.
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WO/2011/119719 |
An aircraft passenger seat assembly includes a seat frame on which is mounted at least one seat back, a seat pan and a plurality of seat legs and at least one seat floor panel having integrated floor panel seat tracks mounted therein and...
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WO/2011/119458 |
A swashplate system includes a rotating outer ring and a non-rotating inner ring, the rotating outer ring being adapted to carry a coil of wire and the non-rotating inner ring being adapted to carry a first and a second magnet. The first...
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WO/2011/113142 |
A system and method is provided for measuring and metering deicing fluid as it is dispensed from a tank onto an aircraft to remove ice and to prevent subsequent icing. The system can include a guided wave radar gauge mounted on the tank ...
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WO/2011/113144 |
An aerial fire suppression system mountable to a helicopter fuselage is provided. The system having a tank divided into at least two compartments by a barrier. The base of each compartment having an outwardly opening door. The system als...
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WO/2011/114635 |
A scheduling system is provided with: a link generating means for generating links, which are partial routes generated as a result of dividing a moving route of a moving body that is indicated in moving-plan data; a link adjustment-latit...
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WO/2011/114278 |
The application discloses an aeronautical input/output device (70) for flight task management which comprises a display unit (90) with a housing (97), and a keyboard unit (91) which is adapted to communicate with the display unit (90). T...
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WO/2011/114426 |
A device for absorbing an impact applied to a moving body, capable of exhibiting high impact absorbing performance for different types of collisions when the moving body collides with an obstacle, etc. A device for absorbing an impact ap...
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WO/2011/113144 |
An aerial fire suppression system mountable to a helicopter fuselage is provided. The system having a tank divided into at least two compartments by a barrier. The base of each compartment having an outwardly opening door. The system als...
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WO/2011/113516 |
The invention relates to a system (10) for controlling a water landing of an aircraft comprising at least one detection device (12, 14, 16, 18), which is designed to detect at least one signal suitable for recognizing an imminent water l...
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WO/2011/115164 |
The disclosed device can compute a high-reliability estimate of aerodynamic coefficients, allowing accurate detection of failure of or damage to control surfaces while reducing the burden on passengers. Said device is provided with: a co...
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WO/2011/115475 |
The present invention relates to a method and apparatus for oscillating a foil in a fluid. The method according to the invention comprises the steps of - generating an oscillating heave motion of the foil in the fluid, the oscillation cy...
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WO/2011/113696 |
An energy-regulating device (2) for regulating hybrid energy sources (E1, E2) for an aircraft is designed to determine an operating characteristic of an energy source (E1, E2), a requirement of a first required resource of at least one f...
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WO/2011/114324 |
A system for landing a VTOL aircraft on a landing platform, comprises a) a net, positioned in a plane substantially parallel to the plane of the landing platform; b) proximity sensors suitable to provide data indicative of the distance a...
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WO/2011/116202 |
A brake system control unit controls one of first and second portions of a wheel brakes electric brake actuators to activate one of the first and second portions of the actuators and deactivate the other during an inhibited braking mode....
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WO/2011/114278 |
The application discloses an aeronautical input/output device (70) for flight task management which comprises a display unit (90) with a housing (97), and a keyboard unit (91) which is adapted to communicate with the display unit (90). T...
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WO/2011/113821 |
Variable pitch mechanism for the blades of a fan (16) of a system of contrarotary fans for a turbomachine, each blade (16a) being able to move about a radial axis (Y), said mechanism comprising a linear actuator, means (56) for convertin...
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WO/2011/114531 |
Ground stations (20, 21) receive an optional signal transmitted from a geostationary artificial satellite (10) and accumulate the received signal with the receiving times thereof. Correlation processing between the received signal by the...
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WO/2011/114147 |
A mobile access unit for allowing passengers to embark or disembark from a craft, such as an aircraft, the unit comprising: a first moveable ramp section (2), extending from an entry/exit end (2a), which allows access to the loading door...
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WO/2011/113880 |
The invention relates to a flexible sheet material for reducing the air drag of an aircraft, in particular an airplane. According to the invention, the flexible sheet material is formed by at least one metal wire assembly, in particular ...
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WO/2011/116171 |
Embodiments of the present invention provide stackable meal trays for use in transporting and heating meal casseroles in an induction oven. The trays have casseroles receiving portions, as well as space - creating features to create a sp...
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WO/2011/114055 |
The invention relates to a device for driving at least one landing gear wheel of an aircraft by means of a wheel motor, which is intended to be used in the stage when the aircraft is traveling on the ground, said aircraft having turbojet...
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WO/2011/115792 |
A latch (10) includes a body (12) having a first end (13) and a second end (15), a trigger-catch-pin (64), and a pin adjustment mechanism (52) for adjusting the position of the trigger-catch-pin (64) within the body (12). The latch (10) ...
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WO/2011/113696 |
An energy-regulating device (2) for regulating hybrid energy sources (E1, E2) for an aircraft is designed to determine an operating characteristic of an energy source (E1, E2), a requirement of a first required resource of at least one f...
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WO/2011/114241 |
The invention relates to the field of aviation and constitutes an aircraft heavier than air. The aircraft uses the effect of the development of lifting force according to the principle of operation of an aeroplane wing and partially uses...
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WO/2011/116202 |
A brake system control unit (60) controls one of first and second portions (86,88) of a wheel brakes electric brake actuators to (70a, b, c, d) activate one of the first and second portions of the actuators and deactivate the other durin...
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WO/2011/112630 |
A ground power unit (14) having a power supply unit capable of accepting a wide range of AC input voltages and producing one or more DC power signals for powering components of the GPU is disclosed. In one embodiment, the power supply un...
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WO/2011/110327 |
A high lift system with a main wing and control flaps, wherein the respective guiding device are at least partially provided with a fairing, having a flow control device for purposes of controlling the flow around the high lift system wi...
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WO/2011/110408 |
The invention relates to the design of water-conducting pipes having an integrated heating system for frost protection and connecting, joining and control elements suitable for said purpose. A self-heating water pipe segment is provided,...
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WO/2011/109842 |
The invention relates to a tank (1) for holding an operating agent for a vehicle, comprising a substantially cylindrical metal casing (2) which is sealed at least at one end by an end cover (3) or end container (4) consisting of injectio...
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WO/2011/112930 |
A method for use with a transmission system (A, A1, B) incorporating a split gear assembly (20, 120, 220) for splitting an applied input load between two or more reaction gears (30, 40, 130, 140, 230, 240) or pathways to selectively posi...
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WO/2011/111226 |
A structure for an aircraft seat section, configured to be able to have an appropriate impact absorbing stroke in an aircraft having a small interior space. The structure is provided with a survival tub (1) which is an occupant protectio...
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WO/2011/110881 |
The invention relates to a fuel tank. The fuel tank is provided with an elastic partition which corresponds to the fuel tank in circumference and shape. The tank is divided into two chambers, a fuel chamber (10) and an excess fuel chambe...
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WO/2011/110555 |
The invention relates to a travelling-wave tube (5) of the type including a radiating collector, in which the tube (5) comprises a collector (6) that extends externally beyond the walls (2, 3) of a device placed in a high-vacuum environm...
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WO/2011/110659 |
The invention relates to a device for determining the operational state of an electro-expulsive deicing system (1) including a current pulse generator (3) and an electro-expulsive mat (2), a sensor (4) connected between the current pulse...
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WO/2011/110408 |
The invention relates to the design of water-conducting pipes having an integrated heating system for frost protection and connecting, joining and control elements suitable for said purpose. A self-heating water pipe segment (100) is pro...
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WO/2011/111405 |
Disclosed are a deicing device for the leading edge of the wing of an aircraft and an aircraft main wing, which are configured by being provided with: a warm air path (46) which is formed along the inside of the curved leading edge (41) ...
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WO/2011/112150 |
Chair for enhancing comfort when required to be seated for long durations, such as in aeroplane, auditorium, theater, waiting lounge, automobile, library and the like. When for use in a public seating arrangement having multiple chairs l...
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WO/2011/110829 |
A stop pad (11) for an aircraft landing gear arranged to provide protection against impact between first and second elements of the landing gear, the stop pad being arranged to provide an indication that it is been subject to an impact a...
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